EP0382290A1 - Méthode et appareil pour la calibration automatique d'un compas à vanne de flux - Google Patents

Méthode et appareil pour la calibration automatique d'un compas à vanne de flux Download PDF

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Publication number
EP0382290A1
EP0382290A1 EP90200226A EP90200226A EP0382290A1 EP 0382290 A1 EP0382290 A1 EP 0382290A1 EP 90200226 A EP90200226 A EP 90200226A EP 90200226 A EP90200226 A EP 90200226A EP 0382290 A1 EP0382290 A1 EP 0382290A1
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EP
European Patent Office
Prior art keywords
characteristic
flux
readings
gate
offset position
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP90200226A
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German (de)
English (en)
Inventor
Richard Wanous
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Magnavox Government and Industrial Electronics Co
Philips North America LLC
Original Assignee
Magnavox Government and Industrial Electronics Co
Magnavox Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Magnavox Government and Industrial Electronics Co, Magnavox Co filed Critical Magnavox Government and Industrial Electronics Co
Publication of EP0382290A1 publication Critical patent/EP0382290A1/fr
Withdrawn legal-status Critical Current

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    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B3/00—Measuring instruments characterised by the use of mechanical techniques
    • G01B3/16—Compasses, i.e. with a pair of pivoted arms
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C17/00—Compasses; Devices for ascertaining true or magnetic north for navigation or surveying purposes
    • G01C17/38—Testing, calibrating, or compensating of compasses

Definitions

  • This invention relates generally to flux-gate compasses and, more particularly, to techniques for calibration of flux-gate com­passes in moving vehicles.
  • a flux-gate compass is a magnetometer by means of which the direction of the earth's magnetic field may be accurately determined.
  • Flux-gate compasses may be usefully employed on any movable platforms, such as land-based vehicles or ships, and may be integrated into complete navigation systems.
  • a flux-gate sensor comprises an annular magnetic core and either two or three coils of wire, each of which is wound diametri­cally about the core. For purposes of explanation, it is easier to assume that there are just two coils, oriented at right-angles to each other.
  • a three-axis magnetometer works on the same principal as the two-axis magnetometer, and there is a mathematical transformation that converts three-axis output signals to the simpler two-axis format. An excitation winding is wrapped about the core at one point in its circumference, and provides a uniform periodic magnetic flux in the core.
  • the voltage output signals, v x and v y , from the two coils, designated with x coil and the y coil, are alternating signals directly proportion­al to sin ⁇ and cos ⁇ , respectively, where ⁇ is the angle between magnetic north and the direc­tion in which the plane of the x coil is aligned.
  • United States Patent No. 4,611,293 to Hatch et al. discloses a technique for calibrating a compass to compensate for these distortions.
  • Part of this tech­nique involves transforming the elliptical characteris­tic to a circle with a radius equal to half the width of the ellipse along its minor axis.
  • the principal drawback of the technique is that the vehicle must be rotated through 360 degrees to perform the calibration. In fact, this is a requirement of all calibration tech­niques prior to the present invention.
  • the permanent magnetism effects that distort the com­pass characteristic are very much dependent on the load carried by the vehicle. If the vehicle loads or unloads a cargo containing magnetic materials, the compass is moved out of calibration. Driving the vehicle in a circle for recalibration may not be convenient, and the compass readings will be suspect until such time as calibration is possible.
  • the present invention resides in a technique for calibrating a flux-gate compass on an automatic and continual basis, without the need for driving in a full circle each time that calibration is necessary.
  • the method of the invention comprises the steps of performing an initial calibra­tion, to determine various parameters distorting the performance characteristic of the compass, and then continuously and automatically revising a significant one of the parameters relating to the effects of per­manent magnetism in the vehicle.
  • the method of the invention includes the steps of performing an initial calibration to determine the proportions, orientation and offset position of an elliptical performance characteristic derived from output signals from a flux-gate compass having a multiple-axis flux sensor installed in a vehicle; transforming the elliptical characteristic to a circular one; obtaining successive sets of readings from the flux-gate compass, for the determination of compass bearings; compensating each of the successive sets of flux-gate readings to conform with the circular characteristic, based on the determinations of the proportions, orientation and offset position of the elliptical characteristic; and revising the determi­nation of the offset position of the elliptical charac­teristic for use in subsequent steps of compensating the flux-gate readings, whereby successive revising steps result in convergence of the offset position on a new value to compensate for changes in permanent magne­tism in the vehicle.
  • the step of per­forming an initial calibration includes rotating the vehicle through a complete circle, taking successive flux-gate readings at successive positions while the vehicle is being rotated, and determining from the readings a set of parameters defining the degree to which the elliptical characteristic is distorted from the corresponding circular characteristic. if the com­pass is a three-axis type, the readings are transformed to equivalent two-axis readings to faciliate further processing.
  • the step of transforming the elliptical characteristic to the cir­cular one includes removing the positional offset of the characteristic, rotating the elliptical characteris­tic, and scaling the elliptical characteristic to con­form with a circle.
  • the step of revising in­cludes determining an measured radius of the circular response characteristic from the readings obtained, determining a correction value by subtracting from the measured radius a previously determined radius, and determining a new offset position for the circular response characteristic, derived from the prior offset position and the correction value determined in the previous step.
  • the method of the invention includes the steps of (a) obtaining two-axis readings from the flux-gate compass; (b) trans­forming the two-axis readings to conform to a circular performance characteristic; (c) determining a measured radius of the circular performance characteristic from the readings obtained in steps (a) and (b); (d) determi­ning a correction value by subtracting from the meas­ured radius a previously determined radius; (e) determi­ning a new offset position for the circular response characteristic, derived from a prior offset position and the correction value determined in step (d); and (f) using the new offset position in the transformation of subsequent compass readings to conform to the circu­lar characteristic.
  • the invention includes means for performing an initial calibration to deter­mine the proportions, orientation and offset position of an elliptical performance characteristic derived from output signals from a flux-gate compass; means for transforming the elliptical characteristic to a cir­cular one; means for obtaining successive sets of read­ings from the flux-gate compass, for the determination of compass bearings; means for compensating each of the successive sets of flux-gate readings to conform with the circular characteristic, based on the determina­tions of the proportions, orientation and offset posi­tion of the elliptical characteristic; and means for revising the determination of the offset position of the elliptical characteristic for use in subsequent steps of compensating the flux-gate readings, whereby successive revisions result in convergence of the off­set position on a new value to compensate for changes in permanent magnetism in the vehicle.
  • the present invention represents a significant improve­ment in the field of flux-gate compasses. Specifically, the improvement provides for automatic calibration of the compass without having to drive the vehicle through a full circle each time the vehicle permanent magnetism is changed.
  • the improvement provides for automatic calibration of the compass without having to drive the vehicle through a full circle each time the vehicle permanent magnetism is changed.
  • the present invention is concerned with a cali­bration technique for flux-gate compasses.
  • Distortions of the former type relating to permanent magnetism of the vehicle, are significantly affected by changes in the vehicle load. It was the discovery of this distinction that led to the present invention, since it appeared that calibration could be performed based only on compensation for displacement of the characteristic from a central position.
  • the elliptical characteristic of FIG. 1 can be convert­ed to a circular characteristic centered at X1, Y1.
  • This transformation is performed in four steps. First the ellipse 10 centered on X1, Y1, as shown in FIG. 1, is transformed to a new set of axes X, Y having their origin at the point X1, Y1 with respect to the X0, Y0 axes, as shown in FIG. 2a. Then the ellipse is effectively rotated about its center until the major axis is aligned with the Y axis and the minor axis is aligned with the X axis, as shown in FIG.
  • FIG. 2d This derived circular characteristic of FIG. 2d has a radius proportional to the magnitude of the earth's magnetic field being measured, and an offset center proportional to the permanent magnetism effects.
  • FIGS. 3a-3d illustrate how this derived cir­cular characteristic is used in accordance with the invention.
  • the solid circle centered at X1, Y1 is the circular equivalent of the elliptical characteristic of the flux-gate compass being cali­brated.
  • the radius 'r' of the circle represents the magnitude of earth's magnetic field as measured by the flux-gate compass, and is a value obtained routinely when the compass is initially calibrated by rotating the vehicle. If the compass is out of calibration due to changes in permanent magnetism, the derived circular characteristic will be displaced to a new location, as indicated, for example, by the broken circle centered at X M , Y M .
  • This new center position is not known or easily measurable, but the technique of the invention is to move the solid circular characteristic continual­ly in such a manner that there will be rapid conver­gence on the new position X M , Y M .
  • the compass will derive a longer "radius.” That is to say, the compass will assume that the radius of the characteristic is the distance from A to the origin X1, Y1. This measured radius is longer than the real radius by an amount ⁇ 1. As will be appre­ciated, for certain headings this difference value will be negative.
  • the compensation action of the invention has the effect of moving the center of the circle along line R1 by an amount ⁇ 1, to a new center point X2, Y2, the point at which the solid circle is centered in FIG. 3b. The compensating action places the solid circle such that the point A is now on the circum­ference of the circle.
  • the solid circle centered at X2, Y2 is closer to the real center X M , Y M , and may be considered as centered at the origin of a new set of axes X′, Y′.
  • the vehicle has a heading conforming to the radial line R2, and a compass reading is derived from point B on the broken circle, which, it will be recalled, is indicative of the observable characteristic of the device.
  • the measured "radius" from the origin X2, Y2 to the point B is longer than the true radius by ⁇ 2. Therefore, the solid circle of FIG. 3b is displaced by ⁇ 2 along the radius R2.
  • the automatic calibration technique of the invention depends on there being an initial calibration step in which the vehicle is rotated through 360 de­grees.
  • This provides raw data corresponding to an ellip­tical characteristic like the one shown in FIG. 1.
  • the elliptical characteristic is transformed to a circular characteristic having a radius 'b' and a center at point X1, Y1 with respect to axes X0, Y0.
  • each new observation of x and y values can be converted to conform to the circular characteristic, using parameters derived in the initial calibration process.
  • H tan ⁇ 1(X A /Y A )
  • the new offset values for the center of the circular characteristic are used in the processing the next measured heading, and the process is repeated.
  • Each new observed heading results in a new correction for the offset coordinates, and there is rapid conver­gence on the new values X M , Y M .
  • the process of calibration is, therefore, automatic and continuous. When a load change renders the current calibration inaccurate, recalibration is achieved in a minute or two, depending on the number of turns made by the vehicle.
  • the three-axis version may be transformed mathematically to the two-axis case, to derive corresponding x and y val­ues from the three output values provided by a three-­axis system.
  • the invention is most conveniently implemented in software or firmware form.
  • the hardware and software needed to perform the initial calibration is fully dis­closed in the aforementioned patent.
  • the additional software needed to perform the ongoing automatic is illustrated in the flowchart of FIG. 4.
  • the present invention represents a significant advance in the field of flux-gate compasses.
  • the invention provides for automatic and continuous calibra­tion for changes in permanent magnetism of the vehicle in which the compass is used.
  • the invention is described, for the most part, in terms relating to a two-axis flux-gate compass, it will be appreciated that the same prin­ciples may be applied to a three-axis flux-gate com­pass, with appropriate transformations of the compass output signals.
  • vehicle is used repeatedly to describe the environment in which the compass of the invention is used, it should be un­derstood that this term is intended to encompass all movable platforms, including ships and aircraft as well as land-based vehicles. Accordingly, the invention is not intended to be limited by the illustrative embodi­ment described in this specification.

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  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Measuring Magnetic Variables (AREA)
  • Navigation (AREA)
EP90200226A 1989-02-06 1990-01-31 Méthode et appareil pour la calibration automatique d'un compas à vanne de flux Withdrawn EP0382290A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US07/306,416 US5046031A (en) 1989-02-06 1989-02-06 Method and apparatus for automatic flux-gate compass calibration
US306416 2002-11-27

Publications (1)

Publication Number Publication Date
EP0382290A1 true EP0382290A1 (fr) 1990-08-16

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EP90200226A Withdrawn EP0382290A1 (fr) 1989-02-06 1990-01-31 Méthode et appareil pour la calibration automatique d'un compas à vanne de flux

Country Status (6)

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US (1) US5046031A (fr)
EP (1) EP0382290A1 (fr)
JP (1) JPH02290508A (fr)
KR (1) KR900013288A (fr)
CA (1) CA2009171A1 (fr)
IL (1) IL93260A0 (fr)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0512317A2 (fr) * 1991-05-10 1992-11-11 VDO Adolf Schindling AG Procédé pour la poursuite de la valeur de correction d'un détecteur attaché à un véhicule
WO1993006434A1 (fr) * 1991-09-17 1993-04-01 Siemens Aktiengesellschaft Procede de compensation d'un champ magnetique perturbateur dans un vehicule
EP0623806A2 (fr) * 1993-05-07 1994-11-09 Lectron Products, Inc. Procédé et appareil d'étallonage d'un système de compas d'un véhicule
WO2004003476A1 (fr) 2002-07-01 2004-01-08 Asahi Kasei Emd Corporation Dispositif et procede de mesure d'azimuts
DE102021210552A1 (de) 2021-09-22 2023-03-23 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung eingetragener Verein Vorrichtung und verfahren zum kalibrieren eines magnetsensorsystems mittels einer inhomogenen magnetfeldquelle

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US5165269A (en) * 1990-10-29 1992-11-24 Iimorrow, Inc. Electronic flux gate compass calibration technique
US5287295A (en) * 1991-05-30 1994-02-15 Motorola Method and apparatus for calibrating an electronic compass to account for alignment errors in the compass windings
JPH051914A (ja) * 1991-06-25 1993-01-08 Pioneer Electron Corp 着磁ベクトル補正方法
US5156038A (en) * 1991-08-01 1992-10-20 Motorola, Inc. Calibration technique for a vehicle's differential odometer
WO1993009509A1 (fr) * 1991-11-01 1993-05-13 Motorola, Inc. Systeme de captage d'une precision amelioree pour la navigation de vehicules
US8352400B2 (en) 1991-12-23 2013-01-08 Hoffberg Steven M Adaptive pattern recognition based controller apparatus and method and human-factored interface therefore
US10361802B1 (en) 1999-02-01 2019-07-23 Blanding Hovenweep, Llc Adaptive pattern recognition based control system and method
US5828984A (en) * 1991-12-27 1998-10-27 Chrysler Corporation Data processing method for an electronic compass system
US5297063A (en) * 1991-12-27 1994-03-22 Chrysler Corporation Method for selecting calibration data for an auto-calibrating compass
JP3316889B2 (ja) * 1992-02-05 2002-08-19 株式会社デンソー 車両用方位検出装置
US5187872A (en) * 1992-04-02 1993-02-23 Her Majesty The Queen In Right Of Canada, As Represented By The Minister Of Communications Automatic calibration of magnetic compasses
US5345382A (en) * 1992-05-15 1994-09-06 Zexel Corporation Calibration method for a relative heading sensor
US5402365A (en) * 1992-10-28 1995-03-28 Motorola, Inc. Differential odometer dynamic calibration method and apparatus therefor
US5737226A (en) * 1995-06-05 1998-04-07 Prince Corporation Vehicle compass system with automatic calibration
US5761094A (en) * 1996-01-18 1998-06-02 Prince Corporation Vehicle compass system
EP0920637A4 (fr) * 1997-01-31 2002-05-29 Greenfield Entpr Inc Procede et systeme de navigation
US7268700B1 (en) 1998-01-27 2007-09-11 Hoffberg Steven M Mobile communication device
US8364136B2 (en) 1999-02-01 2013-01-29 Steven M Hoffberg Mobile system, a method of operating mobile system and a non-transitory computer readable medium for a programmable control of a mobile system
US7966078B2 (en) 1999-02-01 2011-06-21 Steven Hoffberg Network media appliance system and method
US6445178B1 (en) 1999-02-24 2002-09-03 Donnelly Corporation Vehicular magnetic displacement sensor for determining an offset in the output of the sensor
US6513252B1 (en) * 1999-04-08 2003-02-04 Donnelly Corporation Vehicle compass compensation
US6301794B1 (en) * 1999-05-27 2001-10-16 Johnson Controls, Inc. Vehicle compass system with continuous automatic calibration
US6408251B1 (en) 1999-07-29 2002-06-18 Hrl Laboratories, Llc Calibrating a magnetic compass with an angular rate gyroscope and a global positioning system receiver
US6577976B1 (en) 1999-09-17 2003-06-10 Hrl Laboratories, Llc Method for dynamic autocalibration of a multi-sensor tracking system and apparatus incorporating it therein
US6539639B2 (en) * 2000-12-06 2003-04-01 Honeywell International Inc. Monitoring accuracy of an electronic compass
US6651003B2 (en) 2001-07-30 2003-11-18 Innovative Design Solutions, Inc. Method of automatic continuous calibration for an electric compass
JP4141766B2 (ja) * 2002-08-23 2008-08-27 富士通株式会社 照明装置及び液晶表示装置
US6860023B2 (en) * 2002-12-30 2005-03-01 Honeywell International Inc. Methods and apparatus for automatic magnetic compensation
US7260896B2 (en) * 2004-04-07 2007-08-28 Siemens Vdo Automotive Corporation Electronic compass and method of calibration
US7523559B2 (en) * 2004-04-07 2009-04-28 Continental Automotive Systems Us, Inc. Compass heading noise immunity
US7225551B2 (en) 2004-04-07 2007-06-05 Siemens Vdo Automotive Corporation Electronic compass and method for tracking vehicle rotation
US7248983B2 (en) 2004-04-07 2007-07-24 Siemens Vdo Automotive Corporation Electronic compass and method of controlling an electronic compass using independent calibration and compass heading modules
US8577637B2 (en) * 2009-09-28 2013-11-05 Teledyne Rd Instruments, Inc. System and method of magnetic compass calibration
US8825426B2 (en) * 2010-04-09 2014-09-02 CSR Technology Holdings Inc. Method and apparatus for calibrating a magnetic sensor
US8843338B2 (en) 2011-07-29 2014-09-23 Nokia Corporation Processing Data for Calibration
US11313935B2 (en) 2019-09-09 2022-04-26 Apple Inc. In-field soft magnetic distortion hardware compensation

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EP0214817A2 (fr) * 1985-09-03 1987-03-18 British Aerospace Public Limited Company Calibrage d'un compas magnétique
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DE3509548A1 (de) * 1985-03-16 1986-09-18 Robert Bosch Gmbh, 7000 Stuttgart Verfahren zur ermittlung der fahrtrichtung eines fahrzeuges mit elektronischem kompass
EP0214817A2 (fr) * 1985-09-03 1987-03-18 British Aerospace Public Limited Company Calibrage d'un compas magnétique
DE3734057A1 (de) * 1986-10-08 1988-04-21 Mitsubishi Electric Corp Richtungssucher
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Cited By (15)

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Publication number Priority date Publication date Assignee Title
EP0512317A3 (en) * 1991-05-10 1993-03-17 Mannesmann Kienzle Gmbh Method for determining the track of a vehicle using less memory
EP0512317A2 (fr) * 1991-05-10 1992-11-11 VDO Adolf Schindling AG Procédé pour la poursuite de la valeur de correction d'un détecteur attaché à un véhicule
EP0657746A3 (fr) * 1991-09-17 1995-11-22 Siemens Ag Procédé de compensation d'un champ magnétique pertubateur dans un véhicule.
WO1993006434A1 (fr) * 1991-09-17 1993-04-01 Siemens Aktiengesellschaft Procede de compensation d'un champ magnetique perturbateur dans un vehicule
US5581899A (en) * 1991-09-17 1996-12-10 Siemens Aktiengesellschaft Process for compensating a magnetic interference field in a vehicle
EP0657746A2 (fr) * 1991-09-17 1995-06-14 Siemens Aktiengesellschaft Procédé de compensation d'un champ magnétique pertubateur dans un véhicule
EP0623806A2 (fr) * 1993-05-07 1994-11-09 Lectron Products, Inc. Procédé et appareil d'étallonage d'un système de compas d'un véhicule
EP0623806A3 (fr) * 1993-05-07 1994-11-17 Lectron Products, Inc. Procédé et appareil d'étallonage d'un système de compas d'un véhicule
EP0866309A2 (fr) * 1993-05-07 1998-09-23 Lectron Products, Inc. Procédé et appareil d'étallonage d'un système de compas d'un véhicule
EP0866309A3 (fr) * 1993-05-07 1998-12-23 Lectron Products, Inc. Procédé et appareil d'étallonage d'un système de compas d'un véhicule
WO2004003476A1 (fr) 2002-07-01 2004-01-08 Asahi Kasei Emd Corporation Dispositif et procede de mesure d'azimuts
EP1519148A1 (fr) * 2002-07-01 2005-03-30 Asahi Kasei EMD Corporation Dispositif et procede de mesure d'azimuts
EP1519148A4 (fr) * 2002-07-01 2007-07-25 Asahi Kasei Emd Corp Dispositif et procede de mesure d'azimuts
DE102021210552A1 (de) 2021-09-22 2023-03-23 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung eingetragener Verein Vorrichtung und verfahren zum kalibrieren eines magnetsensorsystems mittels einer inhomogenen magnetfeldquelle
DE102021210552B4 (de) 2021-09-22 2023-05-17 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung eingetragener Verein Vorrichtung und verfahren zum kalibrieren eines magnetsensorsystems mittels einer inhomogenen magnetfeldquelle

Also Published As

Publication number Publication date
KR900013288A (ko) 1990-09-05
JPH02290508A (ja) 1990-11-30
IL93260A0 (en) 1990-11-29
US5046031A (en) 1991-09-03
CA2009171A1 (fr) 1990-08-06

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